WO2014143365A1 - Tissé à deux sections entremêlées - Google Patents

Tissé à deux sections entremêlées Download PDF

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Publication number
WO2014143365A1
WO2014143365A1 PCT/US2013/078212 US2013078212W WO2014143365A1 WO 2014143365 A1 WO2014143365 A1 WO 2014143365A1 US 2013078212 W US2013078212 W US 2013078212W WO 2014143365 A1 WO2014143365 A1 WO 2014143365A1
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WO
WIPO (PCT)
Prior art keywords
fibers
woven
section
fringe
layers
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Ceased
Application number
PCT/US2013/078212
Other languages
English (en)
Inventor
Andrew Joseph LAZUR
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Rolls Royce Corp
Original Assignee
Rolls Royce Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Rolls Royce Corp filed Critical Rolls Royce Corp
Priority to EP13826700.0A priority Critical patent/EP2971299B1/fr
Publication of WO2014143365A1 publication Critical patent/WO2014143365A1/fr
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/02—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
    • B32B5/08—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer the fibres or filaments of a layer being of different substances, e.g. conjugate fibres, mixture of different fibres
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
    • B32B3/02—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by features of form at particular places, e.g. in edge regions
    • B32B3/06—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by features of form at particular places, e.g. in edge regions for securing layers together; for attaching the product to another member, e.g. to a support, or to another product, e.g. groove/tongue, interlocking
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/02—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
    • B32B5/022—Non-woven fabric
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/02—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
    • B32B5/024—Woven fabric
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/22—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
    • B32B5/24—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
    • B32B5/26—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
    • B32B7/04—Interconnection of layers
    • D—TEXTILES; PAPER
    • D03—WEAVING
    • D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D1/00—Woven fabrics designed to make specified articles
    • D—TEXTILES; PAPER
    • D03—WEAVING
    • D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D3/00—Woven fabrics characterised by their shape
    • D03D3/04—Endless fabrics
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2250/00—Layers arrangement
    • B32B2250/20—All layers being fibrous or filamentary
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
    • B32B2260/02—Composition of the impregnated, bonded or embedded layer
    • B32B2260/021—Fibrous or filamentary layer
    • B32B2260/023—Two or more layers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
    • B32B2260/04—Impregnation, embedding, or binder material
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
    • B32B2260/04—Impregnation, embedding, or binder material
    • B32B2260/046—Synthetic resin
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/02—Synthetic macromolecular fibres
    • B32B2262/0261—Polyamide fibres
    • B32B2262/0269—Aromatic polyamide fibres
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/10—Inorganic fibres
    • B32B2262/101—Glass fibres
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/10—Inorganic fibres
    • B32B2262/105—Ceramic fibres
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/10—Inorganic fibres
    • B32B2262/106—Carbon fibres, e.g. graphite fibres
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/14—Mixture of at least two fibres made of different materials
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2264/00—Composition or properties of particles which form a particulate layer or are present as additives
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00—Properties of the layers or laminate
    • B32B2307/50—Properties of the layers or laminate having particular mechanical properties
    • B32B2307/58—Cuttability
    • D—TEXTILES; PAPER
    • D10—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10B—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10B2505/00—Industrial
    • D10B2505/02—Reinforcing materials; Prepregs
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/19—Sheets or webs edge spliced or joined
    • Y10T428/192—Sheets or webs coplanar

Definitions

  • the present application relates to joining textile or woven materials, and more particularly but not exclusively, to joining textile or woven materials in a manner configured to provide an interlocking arrangement between the materials.
  • One aspect of the present application is directed to a unique technique for joining textile or woven materials. Other aspects are directed to unique apparatuses, systems, devices, hardware, methods, kits, and/or assemblies related to joining textile or woven materials. Further embodiments, forms, features, aspects, benefits, and advantages of the present application shall become apparent from the description and figures provided herewith.
  • FIGS. 1 -8 are schematic illustrations of various arrangements for joining textile materials.
  • Figures 7A and 7B are schematic illustrations of cross-sectional configurations of fibers in the fringe portions of the textile materials in Figure 6.
  • Figures 8-15 are schematic illustrations of various arrangements for joining textile materials adjacent to a corner of a base form.
  • the textile materials described herein may be used to form a woven structure that includes one or more layers of textile or woven materials, and each layer may include one or more pieces or sections of the textile materials that are joined together.
  • forms in which one or more layers formed from a continuous section of textile material are present with one or more layers that include one or more pieces or sections of the textile materials joined together are also possible.
  • the resultant woven structure may be used as a preform which can be infiltrated with a matrix material to form a composite.
  • matrix materials include polymeric, metallic and ceramic materials.
  • Some exemplary ceramic materials that could be used for the matrix material include silicon carbide, silicon/silicon carbide, and hybrids thereof, just to provide a few non-limiting possibilities.
  • the textile materials may be a 2D fabric, 3D textile, unidirectional fabric, dry non-woven textile, and/or infused or pre- impregnated with binders, and may further include particulates, whiskers, or other fillers.
  • the textile materials may include fibers formed from glass, carbon, aramid, ceramic oxide, ceramic nitride, ceramic carbide such as Nicalon, muliite, alumina, and combinations thereof, just to provide a few examples.
  • a first section 102 of textile material includes a fringe portion 104 and a plurality of fibers 106 and 107, only a few of which have been identified for the sake of clarity.
  • fibers 106 extend in line with longitudinal axis L, although forms in which the orientation of fibers 106 may deviate from that shown in Figure 1 are possible.
  • a second section 108 of textile material includes a fringe portion 1 10 and a plurality of fibers 1 12 and 1 13, only a few of which have been identified for the sake of clarity.
  • Fibers 1 12 extend in line with longitudinal axis L, although forms in which the orientation of fibers 1 12 may deviate from that shown in Figure 1 are possible.
  • a joining portion 1 14 is formed by fringe portions 104, 1 10 to provide an interlocking arrangement between first section 102 and second section 108. More particularly, fibers 106, 1 12 are configured in fringe portions 104, 1 10 in a manner that facilitates formation of joining portion 1 14.
  • a portion of fibers 106, 1 12 is removed along longitudinal axis L in fringe portions 104, 1 10 to enable interlocking in joining portion 1 14 where a number of fibers 106 are positioned adjacent to and overlapping along longitudinal axis L with a number of fibers 1 12. Similarly, a portion of a number of fibers 106 is positioned between a portion of a number of fibers 1 12 and vice versa.
  • the portion of fibers 106, 1 12 that is removed can vary in length and pattern. For an in-plane joining of sections 102, 108, the length of the removed portions of fibers 108,1 12 can vary between a number of different weaving increments taken along longitudinal axis L.
  • the pattern of removed or modified fibers can be one which alternates between fringe portions 104, 1 10 with various repeating patterns. The trimmed fringe length may also be staggered to distribute stress concentration more uniformly.
  • the removed portions of fibers 108, 1 12 have a length along longitudinal axis L that corresponds to a single weaving increment, and alternate in a single pattern between fringe portions 104, 1 10.
  • arrangement 1 14 includes fibers 108, 1 12 in fringe portions 104, 1 10 with portions having a length along longitudinal axis L that corresponds to a 5-unit weaving increment removed in a single alternating pattern between fringe portions 104, 1 10.
  • arrangement 1 15 illustrated in Figure 3 is substantially similar to arrangement 1 14 illustrated in Figure 2.
  • arrangement 1 15 includes a number of support fibers 1 17 positioned in joining portion 1 14.
  • Support fibers 1 17 generally extend transversely, and more particularly
  • support fibers 1 17 can be a group of fibers such as a tow or a monofilament and can vary in material properties from fibers 108, 107, 1 12, and 1 13. The particular properties and parameters of support fibers 1 17 may be selected to maintain a desired fiber volume and/or to add compaction or thickening of joining portion 1 14.
  • Figure 4 illustrates yet another arrangement 1 16, where like numerals refer to like features previously described and the lengths of the removed portions of fibers 106, 1 12 along longitudinal axis L vary. More particularly, six (8) weaving increments are removed from fiber 108 of row 1 18 of fringe portion 104, four (4) weaving increments are removed from fiber 106 of row 120 of fringe portion 104, two (2) weaving increments are removed from fiber 108 of row 122 of fringe portion 104, and no weaving increments are removed from row 124 of fringe portion 104. This pattern repeats through the remaining rows of fibers 106 in fringe portion 104 and alternates with fibers 1 12 of fringe portion 108.
  • first and second sections 102, 108 extend in-line with longitudinal axis L.
  • the ends of first and second sections 102, 108 adjacent to fringe portions 104, 1 10 generally extend orthogonally to longitudinal axis L.
  • forms in which one or both of sections 102, 108 extend transversely to longitudinal axis L and/or the ends of first and second sections 102, 108 adjacent to fringe portions 104, 1 10 do not extend orthogonally to longitudinal axis L are contemplated and possible.
  • portions of fibers 108, 1 12 can be removed in a stepped pattern to match the orientation of the ends of sections 102, 108 relative to one another and longitudinal axis L.
  • Figure 5 illustrates arrangement 126 for joining textile materials that have open weave patterns.
  • the open weave pattern can allow spacing for fibers 108, 1 12 of fringe portions 104,1 10 to interlock when joining portion 1 14 is formed.
  • One or more fibers 108, 1 12 may also be removed in one direction or another on one or both of sections 102, 108.
  • the open weave pattern may also vary in spacing between fibers 108, 1 12 and include fibers in various orientations.
  • section 102 includes fibers 108 which are weaved with cross fibers 128 to provide an open weave 130 between fibers 108 which is approximately the width of fibers 1 12.
  • Section 108 includes fibers 1 12 which are weaved with cross fibers 132 to provide an open weave 134 between fibers 1 12 which is approximately the width of fibers 108.
  • Fibers 106 in fringe portion 104 are positioned in open weave 134 between fibers 1 12 of fringe portion 1 10 and vice versa.
  • Cross fibers 128, 132 which extend perpendicular to fibers 108, 1 12 can be removed from fringe portions 104, 1 10 and support fibers 136 can be placed on either surface of joining portion 1 14 following its formation.
  • one or more of fibers 106, 1 12 can be woven into support fibers 136.
  • cross fibers 128, 132 can be at various orientations and multiple cross fiber orientations can be present in first and second sections 102, 108.
  • support fibers 136 may extend at various orientations and multiple cross fiber orientations can be present in joining portion 1 14. It should also be understood that cross fibers 128, 132 can be removed without placing support fibers 136.
  • cross fibers 128, 132 may be left in place in fringe portions 104, 1 10 and fibers 106, 1 12 can be woven into cross fibers 132, 128, respectively in open weave 130, 134.
  • open weave 130 includes a varied pattern configured to receive a single one of fibers 1 12 at one location and more than one of fibers 1 12 at another location, and fibers 1 12 are correspondingly configured, are also possible. Open weave 134 and fibers 106 could also be provided with this configuration.
  • FIG. 6 Another alternative arrangement 138 for joining sections 102, 108 is illustrated in Figure 6, where like numerals refer to like features previously described, in arrangement 138, the cross-sectional shape or configuration of fibers 108, 1 12 has been modified in fringe portions 104, 1 10, respectively, in order to facilitate formation of joining portion 1 14 without removing material or utilizing an open weave configuration.
  • Non-limiting examples of the modifications that can be made to the cross-sectional shape or configuration of fibers 106, 1 12 in fringe portions 104, 1 10 are illustrated in Figures 7A and 7B.
  • fibers 106, 1 12 initially include a generally oval cross- sectional shape 140 which is reshaped to provide fibers 106, 1 12 with a generally circular cross-sectional shape 142 in fringe portions 104, 1 10.
  • a number of circular openings 144 configured to receive a respective one of reshaped fibers 106, 1 12 are formed.
  • fibers 106, 1 12 initially include a generally oval cross-sectional shape 140 which is reshaped to provide fibers 106, 1 12 with a generally square cross- sectional shape 146 in fringe portions 104, 1 10.
  • a number of square openings 148 configured to receive a respective one of reshaped fibers 106, 1 12 are formed.
  • One non-limiting approach for modifying fibers 106, 1 12 in these manners involves the application of a temporary binder to fibers 106, 1 12 which are then reshaped to create the spaces discussed above. It is also contemplated that forms involving reshaped fibers can also include the removal of portions of fibers 108, 1 12 as discussed above. For example, a joining portion with a taper may be formed by reshaping fibers and removing portions of fibers 106, 1 12 to match the taper of the joining portion.
  • joining portion 1 14 may be the location of a bend, corner or other geometric configuration in a layer formed by sections 102 and 108, and the bend can include any angle between 0° and 180°.
  • a number of fibers 106, 1 12 in fringe portions 104, 1 10 can be provided with a length that allows fibers 106, 1 12 of sections 102, 108 to further extend through and interlock with fibers of one or more additional layers of textile materials positioned over sections 102 and 108.
  • Figure 8 illustrates an arrangement 149 where first and sections 102, 108 are positioned relative to a base form 150 such that joining portion 1 14 is positioned adjacent to corner 151 of base form 150 and is formed at an intersecting angle of less than 180°. Variations in the shape and angle of corner 151 are possible, including forms in which corner 151 is rounded or convexiy curved.
  • a third section 152 of textile material that includes a fringe portion 154 having fibers arranged similar to that of fringe portion 104 for example is positioned over first section 102
  • a fourth section 156 of textile material that includes a fringe portion 158 having fibers arranged similar to that of fringe portion 1 10 for example is positioned over second section 108
  • Fringe portions 154, 158 interlock to provide an arrangement similar to one of those discussed herein above and otherwise form a second joining portion 180.
  • arrangement 149 includes two layers of textile materials; it should be appreciated however that additional layers of textile materials could be present and arranged similar to sections 102, 108, 152 and 156.
  • arrangement 182 illustrated in Figure 9, where like numerals refer to like features previously described, is similar to arrangement 149.
  • arrangement 162 includes a single joining portion 164 formed by fringe portions 104, 1 10 of first and second sections 102, 108 and fringe portions 154, 158 of third and fourth sections 152, 156.
  • the fibers of fringe portions 104, 1 10 are provided with a length that allows them to interlock with the fibers of fringe portions 154, 158 such that joining portion 164 includes an interlocking arrangement between fringe portions 104, 1 10, 154, and 158.
  • the interlocking arrangement of joining portion 164 may be similar to one or more of the arrangements discussed herein above.
  • FIG. 10 illustrates another arrangement 186 that is similar to
  • joining portion 1 14 is elongated relative to its configuration in arrangement 149, and joining portion 180 is offset from and extends obliquely to joining portion 1 14 to form a trailing edge 168.
  • the arrangement shown in Figure 10 may be useful for designs having complex geometry, sharp corners or thick fabric sheets, just to provide a few examples.
  • the interlocking arrangement of fibers from different sections of textile materials allows the joining portion to have a thickness that corresponds to the thickness of a single section of textile material. Further, this thickness of the joining portion is typically one half of what the thickness of the joining portion would be if the sections of textile materials were placed on top of one another without any interlocking
  • Figures 1 1 -15 illustrate alternative arrangements for joining textile materials relative to a corner 172 of a base form 170.
  • corner 172 has a generally linear configuration forming a ninety degree angle, while corner 172 has a curved or radiused configuration in Figure 13.
  • the configuration of comer 172 may further vary in other non-illustrated forms.
  • the arrangements illustrated in Figures 1 1 -15 are exemplary only, and that related arrangements also fail within the scope of the present application.
  • Figure 1 1 illustrates an arrangement 174 that includes a plurality of layers formed by textile sections 178a-h and 178a-178h.
  • Each of sections 176a-h and 178a-h includes a fringe portion similar to one or more of those described herein that facilitates an interlocking arrangement similar to one or more of those discussed above between sections 176a-h and 178a-h that forms a single joining portion 180.
  • the fibers in the fringe portion of each of sections 176a-h extend transversely to the fibers of sections 178a-h and are provided with a length that facilitates interlocking with the fringe portions of sections 178a-h.
  • the fibers in the fringe portion of each of sections 178a-h extend transversely to the fibers of sections 176a-h and are provided with a length that facilitates interlocking with the fringe portions of sections 178a-h.
  • the fibers of the fringe portion of section 178a are configured to extend through and interlock with the fibers in the fringe portion of each of sections 178a-h.
  • Forms in which one or more of sections 176a-h and 178a-h extend through less than each layer present are also possible.
  • Figure 12 illustrates another arrangement 182, where like numerals refer to like features previously described.
  • the fibers of the fringe portions of sections 176a-h and 178a-h do not extend through ail the present layers. Rather, the fringe portions of sections 178a-b and 178a-b interlock and form a first joining portion 184, the fringe portions of sections 176c-d and 178c-d interlock and form a second joining portion 186, the fringe portions of sections 176e-f and 178e-f interlock and form a third joining portion 186, and the fringe portions of sections 178g ⁇ h and 178g-h interlock and form a fourth joining portion 190.
  • comer 172 is generally linear, and joining portions 180 and 184-190 are shown with an angle of incidence between sections 178a-h and sections 178a-h which follows the shape of corner 172. It is contemplated however that the angle of incidence can vary through the arrangement to accommodate various bend features.
  • Figure 13 illustrates yet another arrangement 192, where like numerals refer to like features previously described.
  • a plurality of continuous layers 194 of a material such as a textile material, are positioned adjacent to base form 170 and include a radiused portion 196 that approximates the radius of corner 172.
  • Sections 178a-b and 178a-b are positioned over layers 194 and form a joining portion 198 where an interlocking arrangement is formed by fibers of fringe portions of sections 178a ⁇ b and 178a-b.
  • a filler 200 is placed between layers 194 and sections 176a-b and 178a-b.
  • Filler 200 has a first side geometry 202 that follows the curvature of layers 194 and a second side geometry 204 having a generally linear configuration. Sections 176a-b and 178a-b are shown forming joining portion 198 with an angle of incidence that approximates the shape of second side 204 of filler 200.
  • FIG. 14 illustrates yet another arrangement 206, where like numerals refer to like features previously described.
  • Sections 178a-d and 178a-d are positioned adjacent to base form 170 and the fibers of the fringe portions of these sections interlock to form joining portion 210.
  • Joining portion 210 includes a complimentary shape to corner 172 along an inner portion and a radiused configuration 21 1 along an outer portion.
  • a number of continuous layers 208 of material, such as a textile material, are positioned over sections 178a-d and 178a-d and include an outer radius of curvature 212 that corresponds to radiused configuration 21 1 of joining portion 210.
  • radiused configuration 21 1 can be formed by various approaches including, but not limited to, removal of fibers or portions of fibers by mechanical or thermal processes, selecting certain lengths, or utilizing various weaving patterns.
  • arrangement 214 illustrated in Figure 15, where like numerals refer to like features previously described, is similar to arrangement 206.
  • arrangement 214 includes sections 176e-f and 178e-f positioned over layers 208 and form a joining portion 216 where an interlocking arrangement is formed by fibers of fringe portions of sections 176e-f and 178e-f.
  • a filler 218 is placed between layers 208 and sections 176e-f and 178e-f.
  • Filler 218 has a first side geometry that follows the curvature of layers 208 and a second side geometry having a generally linear configuration. Sections 176e-f and 178e ⁇ f are shown forming joining portion 216 with an angle of incidence that approximates shape of the second side of filler 218.
  • different portions and woven layers of a woven structure can be varied to accommodate various bend features, thicknesses, material properties, outer profiles, and the like. More or fewer woven layers, continuous layers or fabric sheets than shown can be applied.
  • a woven structure in one embodiment, includes a first woven layer and at least a first section and a second section.
  • the first section includes a first fringe portion and a first set of fibers
  • the second section includes a second fringe portion and a second set of fibers.
  • the fibers of the first and second sets of fibers are configured in the first and second fringe to provide an interlocking arrangement between the first and second sections.
  • a system in another embodiment, includes a first woven layer including a first section and a second section.
  • the first section including a first set of fibers extending therefrom and the second section including a second set of fibers extending therefrom, and the first set of fibers extend transversely to and interlock with the second set of fibers adjacent to a corner of a base form.
  • a method in still another embodiment, includes providing a first section of a woven material and a second section of the woven material, and positioning the first section adjacent to the second section with a first number of fibers extending from the first section positioned between a second number of fibers extending from the second section to provide an interlocking arrangement between the first and second sections.

Landscapes

  • Engineering & Computer Science (AREA)
  • Textile Engineering (AREA)
  • Woven Fabrics (AREA)

Abstract

La présente invention concerne des techniques de liaison de matériaux textiles. Selon un aspect de l'invention, un système (100) comprend une structure tissée comportant une première couche tissée et au moins une première section (102) et une seconde section (108). La première section (102) comprend une première partie de frange (104) et un premier ensemble de fibres (106, 107), et la seconde section (108) comprend une seconde partie de frange (110) et un second ensemble de fibres (112, 113). Les fibres des premier et second ensembles de fibres sont organisées dans les première (104) et seconde (110) parties de frange pour fournir une disposition entremêlée entre les première (102) et seconde (108) sections.
PCT/US2013/078212 2013-03-15 2013-12-30 Tissé à deux sections entremêlées Ceased WO2014143365A1 (fr)

Priority Applications (1)

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EP13826700.0A EP2971299B1 (fr) 2013-03-15 2013-12-30 Tissu avec deux sections endentees

Applications Claiming Priority (2)

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US201361790822P 2013-03-15 2013-03-15
US61/790,822 2013-03-15

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WO2014143365A1 true WO2014143365A1 (fr) 2014-09-18

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US12241385B2 (en) * 2023-07-17 2025-03-04 Rtx Corporation Wishbone fiber layup structure for airfoil

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EP0695827A2 (fr) * 1994-06-09 1996-02-07 Albany International Corp. Procédé de jonction de bandes de transfert et autres bandes pour le traitement du papier
WO2003031093A1 (fr) * 2001-10-05 2003-04-17 National Wire Fabric, Inc. Ensemble bande-machine ameliore
EP1897980A1 (fr) * 2006-09-08 2008-03-12 Voith Patent GmbH Bande pour une machine destinée à la fabrication de matériaux en bande, en particulier du papier ou du carton et procédé de fabrication d'une telle bande
FR2970481A1 (fr) * 2011-01-18 2012-07-20 Snecma Structure fibreuse pour piece en materiau composite de geometrie complexe

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US4048277A (en) * 1975-12-15 1977-09-13 Celanese Corporation Splice for use during the thermal stabilization of a flat multifilament band of an acrylic fibrous material comprising at least two segments
DE2902880C2 (de) * 1979-01-25 1985-10-03 Hermann Wangner Gmbh & Co Kg, 7410 Reutlingen Verfahren zum Endlosmachen eines mehrlagigen Entwässerungssiebes und nach diesem Verfahren hergestelltes Entwässerungssieb
US5436042A (en) * 1994-03-11 1995-07-25 The Carborundum Company Ceramic fiber-reinforced composite articles and their production
EP0742185B1 (fr) * 1995-05-10 2000-03-15 Kabushiki Kaisha Toshiba Matériau composité à matrice céramique renforcé par fibres
FI113674B (fi) * 2002-12-18 2004-05-31 Tamfelt Oyj Abp Puristinhuopa
US7943535B2 (en) * 2005-11-17 2011-05-17 Albany Engineered Composites, Inc. Hybrid three-dimensional woven/laminated struts for composite structural applications

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Publication number Priority date Publication date Assignee Title
US4658863A (en) * 1985-03-12 1987-04-21 Binet Feutres S. A. Screen for papermaking press
EP0695827A2 (fr) * 1994-06-09 1996-02-07 Albany International Corp. Procédé de jonction de bandes de transfert et autres bandes pour le traitement du papier
WO2003031093A1 (fr) * 2001-10-05 2003-04-17 National Wire Fabric, Inc. Ensemble bande-machine ameliore
EP1897980A1 (fr) * 2006-09-08 2008-03-12 Voith Patent GmbH Bande pour une machine destinée à la fabrication de matériaux en bande, en particulier du papier ou du carton et procédé de fabrication d'une telle bande
FR2970481A1 (fr) * 2011-01-18 2012-07-20 Snecma Structure fibreuse pour piece en materiau composite de geometrie complexe

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EP2971299B1 (fr) 2020-02-05
US10696008B2 (en) 2020-06-30
US20140272246A1 (en) 2014-09-18
EP2971299A1 (fr) 2016-01-20

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